JPS63154997U - - Google Patents
Info
- Publication number
- JPS63154997U JPS63154997U JP4511587U JP4511587U JPS63154997U JP S63154997 U JPS63154997 U JP S63154997U JP 4511587 U JP4511587 U JP 4511587U JP 4511587 U JP4511587 U JP 4511587U JP S63154997 U JPS63154997 U JP S63154997U
- Authority
- JP
- Japan
- Prior art keywords
- target
- detector
- flying object
- distance
- signal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000010586 diagram Methods 0.000 description 4
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
第１図はこの考案の実施例を示す構成図、第２
図は追尾状態および追尾領域を示す状況図、第３
図は従来の実施例を示す構成図であり、１は飛し
よう体、２は受信アンテナ、３は目標検出器、４
はアンテナ駆動制御部、５は操舵制御部、６は操
舵部、７は目標、８は距離検出器である。なお、
図中、同一符号は同一、又は相当部分を示す。
Figure 1 is a configuration diagram showing an embodiment of this invention, Figure 2
The figure is a situation diagram showing the tracking state and tracking area.
The figure is a configuration diagram showing a conventional embodiment, in which 1 is a flying object, 2 is a receiving antenna, 3 is a target detector, and 4 is a block diagram showing a conventional embodiment.
is an antenna drive control section, 5 is a steering control section, 6 is a steering section, 7 is a target, and 8 is a distance detector. In addition,
In the figures, the same reference numerals indicate the same or corresponding parts.
Claims (1)
目標の位置を検出し、追尾する誘導飛しよう体に
おいて、目標からの反射電波を受信する受信アン
テナと、飛しよう体と目標との距離を検出する距
離検出器と、上記、受信アンテナからの信号によ
つて、目標の位置を識別し、飛しよう体との追尾
角度誤差成分を検出すると共にその検出された角
度誤差信号を、上記、距離検出器から検出された
信号によつて制御が出来る角度検出器と、角度検
出器からの角度誤差信号によつて受信アンテナを
駆動させるアンテナ駆動制御部と、角度検出器か
らの角度誤差信号によつて操舵部を駆動させる操
舵制御部とから構成され、目標までの距離と、追
尾の角度誤差の大きさによつて追尾機能を制御す
ることが出来ることを特徴とする飛しよう体。 By receiving reflected radio waves from the target,
A guided flying object that detects the position of a target and tracks it includes a receiving antenna that receives reflected radio waves from the target, a distance detector that detects the distance between the flying object and the target, and a signal from the above-mentioned receiving antenna. The position of the target is identified, the tracking angle error component with respect to the flying object is detected, and the detected angle error signal can be controlled by the signal detected from the distance detector. Consisting of a detector, an antenna drive control unit that drives a receiving antenna with an angular error signal from the angle detector, and a steering control unit that drives a steering unit with an angular error signal from the angle detector, A flying object characterized in that its tracking function can be controlled depending on the distance to the target and the size of the tracking angle error.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4511587U JPS63154997U (en) | 1987-03-27 | 1987-03-27 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4511587U JPS63154997U (en) | 1987-03-27 | 1987-03-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63154997U true JPS63154997U (en) | 1988-10-12 |
Family
ID=30863561
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4511587U Pending JPS63154997U (en) | 1987-03-27 | 1987-03-27 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63154997U (en) |
-
1987
- 1987-03-27 JP JP4511587U patent/JPS63154997U/ja active Pending
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